INTELSAT 505
Satellite information INTELSAT 505
| Spacetrack Directory Name | INTELSAT 505 |
| Follow INTELSAT 505 | INTELSAT 505 Tracker |
| Pass predictions INTELSAT 505 | Pass predictions INTELSAT 505 |
| Orbit launches |
1982-09-28 (43 years ago)
|
| Days in orbit | 16052 |
| Country/organisation of origin | International Telecommunications Satellite Organization (INTELSAT) (ITSO) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 36220 km |
| Apogee | 36416 km |
| Orbit slope (inclination) | 12.04° |
| Laps per day | 1 |
| Height INTELSAT 505 | 36317.7 km |
Additional information INTELSAT 505
INTELSAT 505, 13595 is a payload satellite owned by INTELSAT (US) in GEO that was launched on Tue, 28 Sep 1982 UTC via an ATLAS SLV-3D CENTAUR launch vehicle from the Air Force Eastern Test Range (AFETR). Payloads include a variety of satellites, spacecraft, and rockets equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
satellite INTELSAT 505 Date of exalting 28.09.1982y. Average height of ISS INTELSAT 505 hundred 36317.7 km. Average velocity INTELSAT 505 is 10999.93 km/h. Inclination INTELSAT 505 satellite 12.06°.TLE
Average velocity INTELSAT 505
Average inclination INTELSAT 505
Mean right ascension of the ascending node (RAAN) INTELSAT 505
Mean argument of perigee INTELSAT 505
Mean semi-major axis of the orbit INTELSAT 505
Mean orbital eccentricity INTELSAT 505
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